04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT BIG-SIZE DEMONSTRATOR
G.A. Amiryants¹, A.V. Chedrik¹, V.A. Malyutin¹, S.E. Paryshev¹, V.G. Soudakov¹; ¹Central Aerohydrodynamic Institute , Russia
The strength requirements and the dynamic stability were provided for the AFLoNext project demonstrator. Another goal was to guarantee high accuracy of measurement of investigated systems efficiency for wing flow control, thanks to the precise account elastic deformations of the demonstrator under the influence of gravity forces and dynamic pressures.